Douglas DC-8-71F
Service difficulty reports · 8,938
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'DC871F' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'DC871F' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS97822829Skin · crackedINSPECTION TYPE-C, R/W CTR L/E BOTTOM INBD AREA IS CRACKED ON BOTH SIDES OF DRAIN HOLE. REPAIRED IAW TIMCO REO NR 03051 AND DC8-57-0777.SDR RRXA97170Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 31R, AT Y=660 TO Y=680. REMOVED AND TREATED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-03061.SDR RRXA97167Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FUSELAGE NOSE SKIN SPLICE DOUBLER, AT Y=8 AND LONGERON 21R. REMOVED AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-03037.SDR UPS97822854Skin · crackedINSPECTION TYPE-C/CK, LEFT WING CENTER LEADING EDGE SECTION CRAKED 2 PLACES, BOTTOM LEADING EDGE BETWEEN ACCESS PANELS DOT E734 DC8-57-0778. CUT AND REMOVED DAMAGED SECTION OF THE 1 AND -27 DOUBLER AREA, FABBED -31 AND -27 AND EXTERNAL DOUBSDR UPS97822568Retract Mech · out of adjustINSPECTION TYPE-N/A ON TAKEOFF CALLED FOR GEAR UP HANDLE WOULD NOT MOVE AT SAME TIME MAIN GEAR SPOILER INOP CAME ON, COMPLETED MAIN SPOILER INOP CHKLST LIGHT WENT OUT, ELECTED NOT TO RAISE GEAR. DUE TO NOISE PREVIOUSLY NOTED. *S/D* PERFORMED ADJ AND TEST OFSDR RRXA97166Keel Cap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION ON LOWER SIDE OF KEEL CAP, AT Y=1040 AND LONGERON 35R. REMOVED AND TREATED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED IAW FAA DER TIMCO ENGINEERING SKETCH REO-03032.SDR RRXA97172Skin · crackedDURING A MAINTENANCE VISIT, FOUND CRACK IN LT INBD FLAP SKIN, AT STA=3.125 LT. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-03027.SDR RRXA97171Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CUSP FITTING, AT Y=70 AND LONGERON 21R. REMOVED AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-03030 AND REO-03037.SDR UPS97822510Engine · flamed outINSPECTION TYPE-N/A, NR 3 ENGINE HAD FLAME-OUT AT FL 330. RAN FLAME-OUT CHECKLIST AND RECOVERED ENGINE AT FL 280 IN DESCENT. *S/D* PERFORMED T/S TREE NR 139, PERFORMED ALL ASPECTS OF ADJ/TEST PER MM 71 -00-00, PERFORMED POWER ASSURANCE RUN AND ALL PMC ON ANSDR RRXA97088Actuator · failedAFTER T/O CREW HEARD LOUD BANG AND SLIGHT A/C SHUDDER, RED GEAR DOOR LIGHT STAYED ON WITH GEAR HANDLE UP AND F/E'S ALTERNATE RIGHT GEAR DOOR LIGHT STAYED ON. (NOTE: BANG OCCURED WHEN GEAR WAS RAISED). MX REMOVED RT GEAR RETRACT CYLINDER, CAPPED HYD LINE, ANDSDR UPS97822855Skin · crackedINSPECTION TYPE-C/CK, LEFT HAND LEADING EDGE WING SECTION OUTBOARD END OF SLOT DOOR CRACKED. REPAIRED IAW REO 03029 AND DC8-57-077.SDR SRAA970402Fire Detector · failedDURING FLIGHT, NR 1 ENGINE FIRE SHORT CIRCUIT LIGHT, MASTER WARNING LIGHT AND FIRE HANDLE LIGHT ILLUMINATED INTERMITTENTLY, ALL OTHER INDICATIONS WERE NORMAL. OBSERVED NR 1 ENGINE AND FOUND NO ABNORMAL CONDITION EXISTS. AIRCRAFT LANDED WITHOUT INCIDENT. FOUSDR IXXA9700031Container · rupturedDURING CLIMBOUT, FUMES WERE NOTED AS THE AIRCRAFT WAS PRESSURIZED. THE AIRCRAFT RETURNED TO OAK FOR AN UNEVENTFUL LANDING. THE SOURCE OF THE FUMES WAS DISCOVERED TO HAVE BEEN A RUPTURED CONTAINER OF ZIOLIN LOCATED IN THE NUMBER ONE CARGO POSITION. THE CONTASDR RRXA97177Frame · gougedDURING A MAINTENANCE VISIT, FOUND GOUGE IN THE FWD CARGO COMPARTMENT BASKET DOOR JAMB, AT Y=333 AND LONGERON 36. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-02988.SDR UPS97822828Spar Cap · crackedINSPECTION TYPE-C, LT MLG WHEEL WELL, WING REAR SPAR LOWER CAP AT FASTENER 6 INCHES OUTBOARD FROM KEEL BEAM STA 857 HAS A CRACK. REMOVED FASTENERS (10) ALONG REAR SPAR AFT SIDE, REAMED DAMAGED HOLE TO .375, CUTOUT CRACKED AREA, FABRICATED REPAIR STRAP, FILLERSDR RRXA97173Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL DOUBLER IN WING LEADING EDGE, AT XFS=17.5 RIGHT WING. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-02979.SDR SRAA970309Actuator Seal · deterioratedAFTER TAKEOFF FOR FLIGHT 128 OUT OF EKCH, DURING GEAR RETRACTION, AIRCRAFT HYDRAULIC QUANTITY INDICATED A RAPID FLUID LOSS. FOLLOWED EMERGENCY PROCEDURE AND SELECTED HYDRAULIC SYSTEM TO STAND BY RUDDER PUMP, AIRCRAFT LANDED SAFELY USING AUXILARY PUMP, INSPECTSDR RRXA97178Frame · gougedDURING A MAINTENANCE VISIT, FOUND GOUGE IN THE AFT CARGO COMPARTMENT BASKET DOOR JAMB, AT Y=1170 AND LONGERON 36. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-02966.SDR RRXA97175Skin · dentedDURING A MAINTENANCE VISIT, FOUND DENT IN THE RT WING UPPER SKIN OF THE FLAP EXHAUST GATE FWD INBD END. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-02969.SDR RRXA97174Skin · crackedDURING A MAINTENANCE VISIT, FOUND LT WING LEADING EDGE SKIN CRACKED, AT XFS=591. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-02970.SDR UPS97822433Battery · dischargedINSPECTION TYPE-N/A, SHIP EMERGENCY BATTERY INOP. REMOVED AND REPLACED SHIPS EMERGENCY BATTERY IAW M/M 34-28-00.SDR UPS97822424Cit Sensor · intermittentINSPECTION TYPE-N/A, NR 1 ENGINE FLAME-OUT AT FL280 W/LIGHT CHOP. ENGINE RESTARTED USING FLAME-OUT CHECKLIST PROCEDURES. PERFORMED FUEL FEED LINE NEG PRESS CH PER MM 28-22-12 SYST HELD PRESS FOUND NO LEAKS. REMOVED AND REPLACED CIT SENSOR IAW 73-20-0, OPS CSDR RRXA97179Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CUSP, AT Y=440 AND LONGERON 21R. REMOVED AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-02945.SDR IXXA9700034Skin · crackedDURING UNSCHEDULED MAINTENANCE VISIT, A CORROSION BULGE AND CRACK OF THE EXTERNAL PLATING WAS FOUND AT FUSELAGE STATION 40, BETWEEN LONGERONS 34 AND 35 RIGHT. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE CORRODED PLATING, FABRICATION AND INSTALLATION OF FINGER DSDR UPS97822403Light · inoperativeINSPECTION TYPE-N/A, EMERG EXIT LIGHT INOP. TIGHTENED OVERHEAD PANEL RECEPTACLE R5-26, OPS CHK SYS NORMAL IAW MM 33-50-02 PG 204-205.SDR UPS97822402Light · inoperativeINSPECTION TYPE-N/A, EMERG LT INOP. REPLACED EMERG BATTERY PACK AND CONTROL RELAY ASSY.SDR UPS97822349Battery Pack · dischargedINSPECTION TYPE-WKD, EMERGENCY EXIT LIGHTS FOUND INOPERATIVE DURING WEEKEND OPERATIONAL CHECK. REMOVED, REPLACED AND TESTED EMERGENCY BATTERY PACK IAW MM 33-50-02.SDR RRXA97075Actuator · failedON GEAR RETRACTION, A LOUD BANG WAS HEARD, GEAR UNSAFE LIGHT ON. MAINTENANCE INSPECTED AND FOUND LEFT MAIN GEAR LOWER RETRACT PIN BROKEN. AIRCRAFT APPROVED FOR FERRY FLIGHT TO MCN FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE LT MAIN LANDING GEAR RETRACTSDR RRXA97073Engine · flamed outAT FL 350, NR 2 ENGINE FLAMED OUT WITH 7.5 IN TANK. PERFORMED ENGINE SHUTDOWN AT FL 200. PERFORMED IN-FLIGHT RELITE, WOULD NOT LITE OFF UNTIL XFEED VALVE OPENED. MAINTENANCE INSPECTED ENGINE FOR DAMAGE, NONE FOUND. VERIFIED FUEL QUANTITY IND SYSTEM FOR ACCSDR IXXA9700030Elevator · jammedDURING TAXI CHECK OF THE ELEVATORS AND POSITION INDICATION SYSTEM, ALL INDICATIONS WERE NORMAL. DURING TAKEOFF ROLL AT 80 KNOTS, THE ELEVATOR CHECK WAS ABNORMAL AND ELEVATOR JAMMED. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT RETURNED TO THE BLOCKS. THE LOCALSDR UPS97822390Door Fitting · crackedINSPECTION TYPE-C, C-3 CARGO DOOR JAMB BACK UP FITTING CRACKED AT BS 1152 LONGERON 33R. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.SDR UPS97822307Hyd Line · looseLOSS OF HYDRAULIC FLUID IN-FLIGHT DOWN TO AUXILIARY LEVEL. (RAPID). FOUND IN RT WHEELWELL LINE ON BRAKE CONTROL VALVE, B-NUT CAME LOOSE. TIGHTENED B-NUT AND LEAK CHECK LINE. NO LEAKS NOTED.SDR UPS97822399Longeron · corrodedINSPECTION TYPE-C, LONG 35L CORRODED BEYOND LIMITS, STA 70 TO 188. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION FROM STA 70 TO 190 PER SRM 51-1-20 AND SRM 51-1-21.SDR UPS97822397Fitting · crackedINSPECTION TYPE-C, TAIL SKID FWD SUPPORT FITTING IS CRACKED AT STA 1756. REPLACED FITTING IAW SRM 51-1-20 AND 51-3-0.SDR UPS97822364Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED AT LOWER AFT END XFS 424.5. REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS97822311Fitting · crackedINSPECTION TYPE: D. INTERCOSTAL END FITTING CRACKED AND CORRODED AT AFT SIDE OF STA 1140 LONGERON 33R. REMOVED AND REPLACED FITTING PER SRM 51-1-20.SDR IXXA9700028Retract Pin · crackedAFTER TAKEOFF AND GEAR RETRACTION, THE GEAR UNSAFE AND DOORS WARNING LIGHTS REMAINED ILLUMINATED AND WOULD NOT EXTINGUISH AFTER CYCLING. FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. GROUND INSPECTION FOUND THE LEFT MAIN LANDING GEAR RETRACT PIN BROKEN.SDR UPS97822351Longeron · corrodedINSPECTION TYPE-C, LONG 36L HAS CORROSION STA 100 TO 190. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21 AND 53-4-1 FIG 28.SDR UPS97822350Doubler · corrodedINSPECTION TYPE-C, BELLY SKIN FINGER DOUBLERS 4 EA CORRODED STA 70 TO 190 STR 31R, 31L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLERS IAW SRM 53-4-1. INSTALLED ON N/R 532668.SDR UPS97822310Fitting · crackedINSPECTION TYPE: D. INTERCOSTAL END FITTING CRACKED, AFT SIDE OF BS 1140 AT LONGERON 35R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DAC DWG 37 58497 AND SRM 51-1-20D.SDR UPS97822309Fitting · crackedINSPECTION TYPE: D. INTERCOSTAL END FITTING CRACKED, AFT SIDE OF BS 1140 AT LONGERON 35L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DAC DWG 3758497 AND SRM 51-1-20D.SDR RRXA97072Directional Gyro · inoperativeAFTER TAKEOFF, FIRST OFFICER'S NR 2 HSI HAD OFF FLAG. AIRCRAFT RETURNED TO KPDX. WHILE ON GROUND NR 2 RMI FAILED AND NR 1 HSI FAILED, BOTH COMPASS SYSTEM HAVE OFF FLAGS. PERFORMED SYSTEM COMPASS CHECK FOUND NR 2 SYSTEM CHECKED GOOD, CAPTAIN'S AND FO'S RMI SDR UPS97822362Skin · corrodedINSPECTION TYPE-C, VERT STAB LE RT CORROSION BLEND OUT IS BEYOND LIMITS, ZFS 140. REMOVED DAMAGE, FABRICATED FILLER, DOUBLER AND INSTALLED IAW SRM 55-2-1, 55-30-01 AND 51-1-11.SDR UPS97822357Longeron · crackedINSPECTION TYPE-C, LONGERON 35R CRACKED AT FASTENER HOLE STA 1540. FABRICATED REPAIR PARTS AND INSTALLED STA 1490 TO 1550 IAW SRM 53-2-2 FIG 10.SDR UPS97822370Fitting · crackedINSPECTION TYPE-C, END FITTING CRACKED AT FS 8 LONG 33R. REMOVED AND REPLACED FITTING IAW SRM 51-1-30 AND 51-1-21.SDR UPS97822366Longeron · crackedINSPECTION TYPE-C, LONGERON 23L CRACKED AT FASTENER HOLE FS 1626. REMOVED, FABRICATED SPLICE SECTION AND INSTALLED IAW SRM 53-2-2 AND 51-1-21.SDR UPS97822341Angle · crackedINSPECTION TYPE-D, LT STUB WING L/E ABOVE NR 1 ENG PYLON INBD ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 9753297, SRM 57-3-1 AND 51-1-21.SDR UPS97822233Clamp · brokenNR 2 ENGINE FIRE WARNING CAME ON, THROTTLE BACK WARNING WENT OUT. FOUND NR 2 ENG HIGH STAGE VALVE CLAMP FAILED. NR 2 ENGINE INBD THRUST REVERSER DAMAGED. REMOVED AND REPLACED NR 2 ENG INBD THRUST REVERSER IAW MM 78-30-00 PN ON CFM56BRO2BRH.SDR UPS97822352Web · crackedINSPECTION TYPE-C, WEB CRACKED AT LBL 60 FS 759 WING TO BODY FAIRING STRUCTURE UNDER SIDE. REPAIRED IAW SRM 53-8-1 AND UPS EO DC8-5350-7876A.SDR UPS97822347Longeron · corrodedINSPECTION TYPE: C. LONGERON 33R CRACKED AND CORRODED F.S. STA 1560. REMOVED, FABRICATED AND INSTALLED IAW SRM 53-2-2 FIG 10 AND 53-4-1.
Back to Douglas DC-8-71F